This booklet is intended for everyone who wants to set the control
parameters of a quadcopter or who works on his own projects with
quadcopters. For anyone who wants to understand why a quadrocopter flies
at all, or how it realizes the self-balancing, and how to choose
controller parameters so that it reaches a predetermined angle of attack
in nick or roll, the reading is recommended. For this purpose, the
flight mechanics is first derived in the chapter 'Physical Model'. This
leads to the simple model of an axis with two motors. So that a
quadcopter can move in one direction, a regulation must be provided
which brings it into an angle of attack. This is dealt with in the 'Axis
Control' chapter. The drift itself is then either controlled visually by
the quadcopter pilot himself or with a superimposed controller that uses
GPS as a sensor. This regulation is dealt with in the chapter 'GPS
Control'. There are many controller structures for quadcopters in the
literature. The one discussed here was deliberately chosen so that it
can be implemented with as many flight controllers as possible. In
particular, the separation into a subordinate axis control and a
superimposed GPS control corresponds to the state of the art in
quadcopter controls.